JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5412' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5412' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2002FA0000193Firewall · crackedDISCOVERED DURING AN ANNUAL INSPECTION THAT THE FIREWALL HAD A 2.75 INCH CRACK AT THE CENTER, LOWER COWL MOUNT DOUBLER. ALMOST IMPOSSIBLE TO VISUALLY DISCOVER WITHOUT KNOWLEDGE OF THE PROBLEM.SDR 2002FA0000191Firewall · crackedIT WAS DISCOVERED DURING AN ANNUAL INSPECTION THAT FIREWALL HAD A 2.75 INCH CRACK AT THE CENTER, LOWER COWL MOUNT DOUBLER. ALMOST IMPOSSIBLE TO VISUALLY DISCOVER WITHOUT KNOWLEDGE OF PROBLEM.SDR 2002FA0000187Firewall · crackedIT WAS DISCOVERED DURING AN ANNUAL INSPECTION THAT THE FIREWALL HAD A 2.75 INCH CRACK AT THE CENTER, LOWER COWL MOUNT DOUBLER. ALMOST IMPOSSIBLE TO VISUALLY DISCOVER W/O KNOWLEDGE OF THE PROBLEM.SDR 2002FA0000186Firewall · crackedDISCOVERED DURING ROUTINE MAINTENANCE THAT THE LEFT LOWER FIREWALL HAD CRACK LOCATED BENEATH THE DOUBLER FOR THE LEFT LOWER COWL MOUNT. IN ONE INSTANCE, CRACK WAS ACTUALLY LOCATED BENEATH THE LEFT FLANGE OF THE BATTERY MOUNT.SDR 2002FA0000138Firewall · crackedIT WAS DISCOVERED DURING ROUTINE MAINTENANCE THAT THE LT LOWER FIREWALL HAD A NEARLY 3 INCH CRACK BENEATH THE CENTER, LOWER COWL MOUNT DOUBLER. THIS CONDITION WAS ALSO DISCOVERED ON THE NEXT FOUR LIKE AIRCRAFT AND THEY WERE ALL CORRECTED IN ACCORDANCE WITH SERSDR USAA020047Bulkhead · crackedCLT - FOUND PYLON MID BULKHEAD WITH .125 INCH CRACK, OUTBOARD SIDE MID BULKHEAD, BOTTOM HOLE. FABRICATED DOUBLER AND SHIMS, VERIFY NO OTHER CRACKS, INSTALLED PE EA 63980A. (M)SDR CA020128004Doubler · cracked(CAN) THE LOWER FWD DOUBLER IS SITUATED ON BOTTOM OF FIREWALL & SUPPORTS NOSEGEAR SPRING ATTACH. DOUBLER FOUND CRACKED ON ITS LT WEB NEAR BOTTOM.SDR FPI2002F00006Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL. CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.SDR FPI2002F00005Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL, CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.SDR QXEA0200065Firewall · crackedPDX - AFT FIRE WALL OUTBOARD SIDE HAS CRACK AT Z100, YN12-0. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.SDR QXEA0200042Firewall · crackedPDX - NR 1 ENGINE FIREWALL CRACKED .25 INCH ABOVE FIRE LOOP SUPPORT BRACKET. REPAIRED IAW DHC-8 RD 8-54-611.SDR QXEA0102131Firewall · crackedPDX - NR 2 ENGINE AFT FIREWALL IS CRACKED AT ABOUT 10:00 AT Z-BRACKET. REPAIRED IAW RD 8-54-611.SDR QXEA0102037Firewall · crackedPDX - NR 1 ENGINE AFT FIRE WALL AT ABOUT THE 11:00 POSITION FOUND A CRACK IN THE FIRE LOOP AREA. REPAIRED IAW RD 8-54-109.SDR USAA011383Bulkhead · crackedCLT - FOUND PYLON MID BULKHEAD .5 INCH, NR 1 PYLON, MID BULKHEAD LOWER BOLT HOLE OUTBOARD. INSTALLED DOUBLER REPAIR PER EA NR 85691 AND 85692. (M)SDR CA011211011Seal · missing(CAN) DURING SCHEDULED MOD PROGRAM IT WAS NOTED THAT THERE WAS A GAPPING CONDITION AT THE ENGINE FUEL AND HYDRAULIC LINES AT THE FIREWALL FAIRLEADS. THERE WERE VISIBLE GAPS BETWEEN SOME OF THE FAIRLEAD SECTIONS AND AROUND SOME OF THE FUEL AND HYDRAULIC LINES ASDR AUS20011241Beam · corroded(AUS) ENGINE BEAMS AND CANTED BULKHEADS CORRODED BEYOND LIMITS. FOUND DURING NDT INSPECTION.SDR 0104466642Bulkhead · crackedDuring "H" check found 2 1/4 inch crack in number 3 pylon rear engine mount bulkhead frame assembly. Repaired per EA 66-185922.SDR QXEA0101774Firewall · crackedPDX - CRACK IN FIREWALL SKIN FROM EDGE TO BOTTOM INBOARD HOLE THAT MATES CLOSING MEMBER P/N 85410449. REPAIRED IAW HORIZON EA 2-54-111.SDR DHL2001801552FittingAFT BULKHEAD JOINT FITTING CRACKED 1/2 IN AT STA 7266.000 AT L176.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.SDR QXEA0101678Firewall · chafedPDX - CHAFE IN NR 2 NACELLE FIREWALL FLANGE APPROXIMATELY 3 INCHES ABOVE LOWER SUPPORT STRUT 6 INCHES LONG AND APPROXIMATELY .020 INCH DEEP. INSTALLED REPAIR DOUBLER IAW EA 2-54-106.SDR QXEA0101684Firewall · crackedPDX - NR 2 ENGINE NACELLE FIREWALL HAS A CRACK ABOVE THE TWO ATTACH RIVETS THROUGH THE INBOARD WALL OF THE CLOSING MEMBER. REPAIRED IAW RD 8-54-109.SDR DL76S011650Bulkhead · crackedDURING ACCOMPLISHMENT OF PYLON SIP MOD, CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD LAYER. REPAIR ER/A 398051-14AD.SDR HEEA076264Firewall · looseAFT ENGINE FIRE WALL ATTACHMENT FLANGE RIVETS LOOSE.SDR QXEA0101646Heat Shield · chafedPDX - RIGHT NACELLE OUTBOARD DISHED HEAT SHIELD CHAFED TOP OF FINGERNAIL DECK. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1.SDR QXEA0101598Firewall · crackedPDX - AFT FIRE WALL IS CRACKED AT CONNECTING CLIP ON TOP INBOARD SIDE. REPAIRED IAW RD8-54-109SDR QXEA0101597Firewall · crackedPDX - AFT FIREWALL IS CRACKED AT TOP INBOARD SIDE APPROXIMATELY 3" LONG ON NUMBER ONE SIDE. REPAIRED IAW RD8-54-806SDR QXEA0101582Firewall · crackedPDX - RIGHT-HAND NACELLE OUTBOARD SIDE AFT FIRE WALL HAS A 2 INCH CRACK BETWEEN THE FIRE LOOP BRACKET AND SUPPORT. REPAIRED IAW RD 8-54-806.SDR QXEA0101421Bulkhead · crackedPDX - 1 INCH CRACK ON NACELLE BULKHEAD AT STATION XN125.5, ZN1.0, AND YW 143.0 (VIEWED LOOKING IN THROUGH 416AR). REPAIRED DAMAGE IAW DASH-8 RD 8-54-611SDR QXEA0101422Bulkhead · crackedPDX - 3/4 INCH CRACK ON CLOSING MEMBER 85410449. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE OUT OF .016 TITANIUM AND INSTALLED IAW E.A. 2-54-98 AND RD 8-54-611.SDR MWEA011199Bulkhead · crackedRIGHT SIDE PYLON BULKHEAD WALL HAS A CRACK IN WEB AT STATION 965 AROUND RIVET FOR SNAP NEAR CENTER OF WALL. FABRICATED AND INSTALLED DOUBLER.SDR DL767011324Bulkhead · crackedDURING ACCOMPLISHMENT OF PYLON SIP MODIFICATION,CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD IN AREA COMMON TO THE UPPER SPAR FITTING.SDR QXEA0101302Firewall · crackedPDX-NACELLE NR 2 HAS A 3/4 INCH CRACK IN FIREWALL ON OUTBOARD SIDE NEXT TO TOP AFT CORNER OF IGNITOR DOOR. REPAIRED IAW RD8-54-806SDR DHL2001363013Bulkhead · corrodedA CHECK--CORROSION AT LWR SURFACE AT NR 1 PYLON LWR BULKHEAD AFT OF ENGINE MOUNT SHIM PLATE. REMOVED CORROSION FROM LOWER SURFACE AT NR 1 PYLON AFT OF ENGINE MOUNT SHIM PLATE IAW A300 SRM 51-40-11SDR AWXA0002128Firewall · damagedE1 HYDRAULIC PRESSURE LINE AT TRANSITION THOUGH PYLON, LOOSE; NR 1PYLON. REPAIRED NR 1 ENG FIRE WALL PYLON IAW ER 15-5412-01202-DL1.SDR QXEA0101161Firewall · crackedPDX - LEFT-HAND NACELLE STAINLESS EXHAUST FIREWALL IS CRACKED ON UPPER RIGHT-HAND SIDE BY UPLOCK ACTUATOR BRACKET MOUNT BOLTS. REPAIRED IAW RD 8-54-806.SDR QXEA0101118Firewall · crackedPDX - RIGHT-HAND NACELLE FIREWALL CRACKED OUTBOARD OF EXHAUST DUCT APPROXIMATELY 10 O'CLOCK POSITION. REPAIRED IAW DHC-8 RD 8-54-806.SDR UIEA01059Bulkhead · crackedDURING INSPECTION OF NR 4 PYLON, FOUND THE REAR ENGINE MOUNT BULKHEAD UPPER T-CHORD L/S CRACKED (R/S PREVIOUSLY REPAIRED). TRIMMED CRACK AREA AWAY. OVERSIZED HOLES IN AFFECTED AREA. HFEC INSPECTED HOLES TO ENSURE CRACK FREE AREA. NO CRACKS FOUND. INSTALLESDR MWEA010778Bulkhead · crackedRIGHT PYLON BULKHEAD WEB WALL AT STATION 965 IS CRACKED APPROXIMATELY 8 INCHES LONG OUTBOARD FROM FLOOR LINE UP. CUT OUT DAMAGED WEB, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB.SDR 20010418CW002Fastener · looseOWNER REPORTED 2 LOOSE RIVETS AT THE FIREWALL ATTACH POINT STA. 5. INVESTIGATION REVEALED 2 MISSING RIVET HEADS AN426AD4 AND A FURTHER 25 RIVET HEADS HELD ON BY PAINT ALONE. 1 OTHER RIVET HEAD HAD A STRANGE APPEARANCE, SCRAPING THE PAINT OFF REVEALED A BONSDR 2001UALA00462Bulkhead · damagedNR 2 PYLON AFT BULKHEAD NACELLE STA 201.02 RIGHT HAND SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. FABRICATED AND INSTALLED REPAIR CRES PLATES. MAJOR REPAIR ACCOMPLISHED.SDR EIA2001131Bulkhead · crackedHKG-HAECO - NR 2 PYLON REAR ENGINE MOUNT BULKHEAD WEB CRACKED AT FORWARD AND AFT SIDE. STOP DRILLED CRACKS, NDT INSPECTED, INSTALLED NEW ANGLE CHORD AND OVERSIZED HI-LOCKS PER BOEING MSGSDR EIA2001127Bulkhead · crackedHKG-HAECO - NR 4 STRUT REAR ENGINE MOUNT BULKHEAD FORWARD SIDE OF FRAME WEB CRACKED AT OUTBOARD LOWER AREA, ADJACENT TO REPAIR ANGLE, APPROX .375 INCH LENGTH. REPAIRED BULKHEAD WEB PER RS R-54-53-34641. CONTINUE DETAIL VISUAL AND HFEC INSPECTION PER SB 747-5SDR EIA2001126Bulkhead · crackedHKG-HAECO - NR 3 STRUT REAR ENGINE MOUNT BULKHEAD AFT SIDE OF FRAME WEB CRACKED AT OUTBOARD LOWER AREA ADJACENT TO REPAIR ANGLE, APPROX .375 INCH LENGTH. STOP DRILLED HOE PER SRM 51-10-01. INSPECT STOP DRILLED HOLE BY HFEC EVERY 600 FLT CYCLES PER SB 747-54ASDR EIA2001125Bulkhead · crackedHKG-HAECO - FOUND 4 CRACKS AT NR 2 ENGINE STRUT REAR ENGINE MOUNT BULKHEAD WEB, FROM FRAME WEB ADJACENT TO REPAIR ANGLE, 1 AT FORWARD SIDE AND 3 AT AFT SIDE. REPAIRED BULKHEAD WEB PER RS R-54-53-34641. CONTINUE DETAIL VISUAL AND HFEC INSPECTION OF B/H IAW SBSDR 2001UALA00283Bulkhead · wornNR 2 PYLON AFT BULKHEAD NAC STA 201.02 RIGHT SIDE VERTICAL FLANGE LOWER CORNER HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR PLATE PER SRM.SDR 2001UALA00217Bulkhead · crackedMAJOR REPAIR. NR 1 PYLON INNER WEB CASTING AT NAC STA 191.86 IS CRACKED AND DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED BULKHEAD.SDR C2XA01TY030Heat Shield · gougedTYS DURING A SCHEDULED INSPECTION THE APU FIREWALL HEAT BLANKET WAS FOUND GOUGED AT THE BLEED VALVE MOUNT BRACKET. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL HEAT BLANKET IAW EMB-145 SB 145-53-0004. REPAIR WAS SATISFACTORY, AIRCRAFT WILL BE RELEASED SDR ABXA010070Bulkhead · crackedA WEB WAS CRACKED AT FUSELAGE STATION 1114 LONGERON 12R. MAINTENANCE INSPECTED AND REPLACED THE WEB IAW DC-9 SRM.SDR MWEA010175Web · crackedLEFT FUSELAGE BULKHEAD SKIN WEB AT PYLON FRONT SPAR BELOW LONGERON 17 IS CRACKED, APPROXIMATELY 6 INCHES OF FUSELAGE SKIN AND JUST ABOVE FLOOR LINE. REMOVED WEB, FABRICATED AND INSTALLED WEB AND STIFFENER.SDR AWXA0001390Bulkhead · crackedNR 1 PYLON NSA 290 AFT ELECTRICAL SUPPORT BULKHEAD CRACKED. REMOVED, FABED, AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-30-01 FIG 7.
Back to JASC 5412